# Service difficulty reports: N15730, cancelled Oct 25, 2007 A list on [N15730, cancelled Oct 25, 2007](https://openairdocs.org/deregistered/N15730-2007-10-25.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 79 reports - [SDR C2XA01IA325](https://openairdocs.org/sdr/C2XA01IA325.md): Controller · inoperative · Aug 10, 2001 · N15730 · Emb EMB120ER · Cabin Pressure Control System > IAH - FLIGHT 3284, THE CREW REPORTED THAT THE AIRCRAFT LOST ALL PRESSURIZATION AT 19000 FEET. THE CREW DESCENDED TO 9000 FEET IN AUTO MODE, AND THE AIRCRAFT SLOWLY BEGAN PRESSURIZING. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND RE - [SDR C2XA01IA215](https://openairdocs.org/sdr/C2XA01IA215.md): Battery Pack · discharged · Apr 11, 2001 · N15730 · Emb EMB120ER · Emergency Lighting > IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT SEVERAL EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XAO1IA210](https://openairdocs.org/sdr/C2XAO1IA210.md): Battery Pack · discharged · Apr 11, 2001 · N15730 · Emb EMB120ER · Emergency Lighting > IAHH - DURING POST-FLIGHT INSPECTION, THE CREW REPORTED SEVERAL EMERGENCY EXIT LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA01IA116](https://openairdocs.org/sdr/C2XA01IA116.md): Mount · burned · Feb 21, 2001 · N15730 · Emb EMB120ER · DC Power Distribution System > IAH - FLIGHT 3551, THE CREW REPORTED THAT WHILE CLIMBING THROUGHT 6000 FEET THE COCKPIT BEGAN TO SMELL LIKE SMOKE FOLLOWED BY A RIGHT PACK FAIL MESSAGE AND A COMPLETE LOSS OF PRESSURIZATION CONTROL. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDEN - [SDR C2XA01IA076](https://openairdocs.org/sdr/C2XA01IA076.md): Circuit Breaker · tripped · Feb 6, 2001 · N15730 · Emb EMB120ER · Air Distribution Fan > SHV - FLIGHT 3525, THE CREW REPORTED A SMOKE SMELL IN THE CABIN AREA. THE AIRCRAFT LANDED AT SHV WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE AVIONICS COOLING FAN CIRCUIT BREAKER TO BE POPPED. MAINTENANCE RESET THE CIRCUIT BREAKER, - [SDR C2XA01IA039](https://openairdocs.org/sdr/C2XA01IA039.md): Actuator · out of adj · Jan 20, 2001 · N15730 · Emb EMB120ER · Landing Gear Actuator > IAH - FLIGHT 3490, THE CREW REPORTED THAT THE RIGHT MAIN LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE RIGHT MAIN LANDING GEAR ACTUATOR TO BE OUT - [SDR C2XA01IA034](https://openairdocs.org/sdr/C2XA01IA034.md): O-Ring · cracked · Jan 14, 2001 · N15730 · Emb EMB120ER · Turbine Engine Oil System > IAH - FLIGHT 2908, THE CREW REPORTED THAT THE NUMBER TWO ENGINE LOST OIL PRESSURE IN FLIGHT WITH A LARGE VISUAL OIL LOSS ON THE RIGHT SIDE OF THE AIRCRAFT. THE CREW SHUTDOWN THE NUMBER TWO ENGINE BEFORE 40 PSID, AND RETURNED TO IAH WHERE IT LANDED WITHOUT INC - [SDR C2XA00IA477](https://openairdocs.org/sdr/C2XA00IA477.md): Hinge · broken · Dec 25, 2000 · N15730 · Emb EMB120RT · Landing Gear Doors > IAH - FLT 2905 - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THE LEFT OUTBOARD AFT MAIN LANDING GEAR DOOR, AFT HINGE WAS BROKEN. MAINTENANCE REMOVED AND REPLACED THE HINGE IAW EMB-120 MM 52-81-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA00CL056](https://openairdocs.org/sdr/C2XA00CL056.md): Proximity Switch · worn · Jul 25, 2000 · N15730 · Emb EMB120RT · Landing Gear Position and Warning > CLE - FLT 3508 - THE LEFT MAIN GEAR WOULD NOT RETRACT (RECYCLED TWICE AND GEAR CAME UP) BOTH GREEN LIGHTS EXTINGUISHED AND BOTH RED REMAINED ILLUMINATED. WIND NOISE COULD BE HEARD FROM LEFT MAIN. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LEFT MAIN GEAR - [SDR C2XA00CL055](https://openairdocs.org/sdr/C2XA00CL055.md): Hinge · worn · Jul 24, 2000 · N15730 · Emb EMB120RT · Landing Gear Doors > CLE - FLT 3121 - THE LEFT MAIN GEAR WOULD NOT RETRACT (RECYCLED TWICE AND GEAR CAME UP) BOTH GREEN LIGHTS EXTINGUISHED AND BOTH RED REMAINED ILLUMINATED. WIND NOISE COULD BE HEARD FROM LEFT MAIN. MAINTENANCE INSPECTED AND REMOVED AND REPLACED FORWARD AND AFT - [SDR C2XA99CL129](https://openairdocs.org/sdr/C2XA99CL129.md): Control Panel · failed · Dec 18, 1999 · N15730 · Emb EMB120RT · Landing Gear Retraction/Extension System > CLE - FLT 3061 - AFTER TAKEOFF FROM CLE, THE LEFT MAN GEAR GREEN LIGHT REMAINED ILLUMINATED (A-SYSTEM). THE CREW CYCLED THE GEAR AGAIN AND GREEN LIGHT STAYED ILLUMINATED. AIRCRAFT RETUREND TO CLE WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED TH - [SDR C2XA99IA354](https://openairdocs.org/sdr/C2XA99IA354.md): Fan Muffler · damaged · Jul 12, 1999 · N15730 · Emb EMB120RT · Air Distribution Fan > IAH - FLT 3561 - THE CREW REPORTED SMOKE IN THE CABIN AFTER NR 2 ENGINE START. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE GASPER FAN ON MEL 21-24-1C CONTROL NR 183333, AND THE AIRCRAFT WAS RETURNED TO SERVICE AND THE AIRCRAFT THEN ABORTED ITS TAKEOFF W - [SDR C2XA99IA331](https://openairdocs.org/sdr/C2XA99IA331.md): Cooling Turbine · inoperative · Jun 16, 1999 · N15730 · Emb EMB120RT · Cabin Cooling System > IAH - FLT 3578 - THE CREW REPORTED SMOKE IN THE CABIN. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT COOLING TURBINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA99IA313](https://openairdocs.org/sdr/C2XA99IA313.md): Bolt · worn · Jun 14, 1999 · N15730 · Emb EMB120RT · Cabin Cooling System > IAH - FLT 3561 - DURING CLIMB, THE CREW REPORTED SMOKE IN THE AIRCRAFT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RAM AIR DOOR ACTUATOR ATTACH BOLT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98CL087](https://openairdocs.org/sdr/C2XA98CL087.md): Actuator · malfunctioned · Dec 28, 1998 · N15730 · Emb EMB120RT · Trailing Edge Flap Actuator > CLE - FLT 3114 - CREW REPORTED THAT THEY RECEIVED A CONTROL FAULT WITH FLAPS AND A ADV SWS ON MAP UPON BRINGING FLAPS FROM 15 DEGREES TO 0 DEGREES, SYSTEM WOULD NOT RESET. MAINTENANCE REMOVED AND REPLACED THE LEFT OUTBOARD FLAP ACTUATOR IAW EMB-120 MM 27-50-0 - [SDR C2XA98CL088](https://openairdocs.org/sdr/C2XA98CL088.md): Control Unit · malfunctioned · Dec 26, 1998 · N15730 · Emb EMB120RT · Trailing Flap Position Indicating System > CLE - FLT 3210 - CREW REPORTED THAT THEY RECEIVED A CONTROL FAULT DURING FLAP RETRACTION AND IT WOULD NOT RESET UNTIL OUTBOARD FLAPS WERE DRIVEN UP BY THE OVERRIDE SWITCH, ALSO WHEN FLAPS WERE SELECTED FOR LANDING THEY DID NOT MOVE. AIRCRAFT LANDED WITHOUT FU - [SDR C2XA98IA400](https://openairdocs.org/sdr/C2XA98IA400.md): Socket · dirty · Oct 2, 1998 · N15730 · Emb EMB120RT · Emergency Lighting > IAH - DURING PREFLIGHT INSPECTION, THE FORWARD LEFT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE CLEANED THE LIGHT SOCKET AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA394](https://openairdocs.org/sdr/C2XA98IA394.md): Tee · corroded · Sep 23, 1998 · N15730 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT T-PROFILE AT FRAME 44 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE T-PROFILE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA393](https://openairdocs.org/sdr/C2XA98IA393.md): Support · cracked · Sep 23, 1998 · N15730 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICLE SUPPORT AT FRAME 13 WAS FOUND TO BE CRACKED. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA392](https://openairdocs.org/sdr/C2XA98IA392.md): Angle · cracked · Sep 23, 1998 · N15730 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICLE SUPPORT ATTACH ANGLE AT FRAME 13 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA391](https://openairdocs.org/sdr/C2XA98IA391.md): Support · cracked · Sep 23, 1998 · N15730 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT VERTICLE SUPPORT AT FRAME 13 WAS FOUND TO BE CRACKED. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA390](https://openairdocs.org/sdr/C2XA98IA390.md): Angle · cracked · Sep 23, 1998 · N15730 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FRAME 13 LEFT VERTICLE SUPPORT ATTACH ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLES IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA389](https://openairdocs.org/sdr/C2XA98IA389.md): Tee · corroded · Sep 23, 1998 · N15730 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT T-PROFILE WAS FOUND TO BE CORRODED AT FRAME 36. MAINTENANCE REMOVED AND REPLACED THE T-PROFILE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA388](https://openairdocs.org/sdr/C2XA98IA388.md): Tee · corroded · Sep 23, 1998 · N15730 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT T-PROFILE AT FRAME 40 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PROFILE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA387](https://openairdocs.org/sdr/C2XA98IA387.md): Beam · corroded · Sep 23, 1998 · N15730 · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING C-CHECK INSPECTION, THE RIGHT CREASE BEAM WAS FOUND TO BE CORRODED FROM FRAME 44 TO FRAME 47. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF CREASE BEAM IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA386](https://openairdocs.org/sdr/C2XA98IA386.md): Strap · corroded · Sep 23, 1998 · N15730 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT BUTT STRAP WAS FOUND TO BE CORRODED AT FRAME 43. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA385](https://openairdocs.org/sdr/C2XA98IA385.md): Tee · corroded · Sep 23, 1998 · N15730 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT T-PROFILE AT FRAME 44 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE T-PROFILE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA384](https://openairdocs.org/sdr/C2XA98IA384.md): Beam · corroded · Sep 23, 1998 · N15730 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT CREASE BEAM WAS FOUND TO BE CORRODED FROM FRAME 38 TO FRAME 44. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA383](https://openairdocs.org/sdr/C2XA98IA383.md): Strap · corroded · Sep 23, 1998 · N15730 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT BUTT STRAP WAS FOUND TO BE CORRODED FROM FRAME 33 TO FRAME 44. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IAW EMB120 SRM 41-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA382](https://openairdocs.org/sdr/C2XA98IA382.md): Bracket · cracked · Sep 23, 1998 · N15730 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT WING TO FUSELAGE FAIRING 193 LOWER SUPPORT BRACKET WAS FOUND TO BE CRACEKED AT THE FORWARD END. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A DOUBLER REPAIR IAW EMB-120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED - [SDR C2XA98IA381](https://openairdocs.org/sdr/C2XA98IA381.md): Strap · corroded · Sep 23, 1998 · N15730 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND LEFT SIDE FLOORBEAM BUTT-STRAP CORRODED BETWEEN FRAME 42 AND 44. MAINTENANCE REMOVED THE DAMAGED SECTION AND REPLACED WITH NEW SECTION IAW EMB-120 SRM 51-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA380](https://openairdocs.org/sdr/C2XA98IA380.md): Strap · corroded · Sep 23, 1998 · N15730 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND RIGHT FLOORBEAM BUTT-STRAP CORRODED AFT OF FRAME 38. MAINTENANCE REMOVED THE DAMAGED SECTION AND INSTALLED REPAIR DOUBLER IAW EMB-120 SRM 51-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA379](https://openairdocs.org/sdr/C2XA98IA379.md): Angle · cracked · Sep 23, 1998 · N15730 · Emb EMB120RT · Vertical Stabilizer > IAH - DURING C-CHECK INSPECTION, FOUND VERTICAL STABILIZER LEFT SIDE DRAG ANGLE CRACKED. MAINTENANCE REMOVED THE DAMAGED FORWARD SECTION AND REPLACED IT IAW CONTINENTAL EXPERSS ENGINEERING CHANGE/REPAIR AUTHORIZATION (ECRA) EC5530-01013. THE AIRCRAFT WAS APPR - [SDR C2XA98IA378](https://openairdocs.org/sdr/C2XA98IA378.md): Frame · cracked · Sep 23, 1998 · N15730 · Emb EMB120RT · Nacelle/Pylon, Main Frame > IAH - DURING C-CHECK INSPECTION, FOUND RIGHT AFT MAIN LANDING GEAR DOOR INBOARD FORWARD HINGE POINT, AFT NACELLE HALF FRAME CRACKED. MAINTENANCE REMOVED AND REPLACED THE HALF FRAME IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ( - [SDR C2XA98IA377](https://openairdocs.org/sdr/C2XA98IA377.md): Rib · cracked · Sep 23, 1998 · N15730 · Emb EMB120RT · Trailing Edge Flaps > IAH - DURING C-CHECK INSPECTION, FOUND LEFT NACELLE FLAP CENTER RIB CRACKED. MAINTENANCE REMOVED AND REPLACED THE FLAP IAW EMB-120 MM 27-50-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA376](https://openairdocs.org/sdr/C2XA98IA376.md): Support · cracked · Sep 23, 1998 · N15730 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND RIGHT NACELLE FLAP CENTER SKIN SUPPORT CRACKED ON UPPER SIDE. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA375](https://openairdocs.org/sdr/C2XA98IA375.md): Support · cracked · Sep 23, 1998 · N15730 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER SKIN SUPPORT FORWARD OF ACCESS 522EB CUTOUT ON RIB 8 CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA374](https://openairdocs.org/sdr/C2XA98IA374.md): Angle · cracked · Sep 23, 1998 · N15730 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING RIB 8 TO STRINGER 11 SUPPORT ANGLE CRACKED. MAINTENANCE REMOVED AND REPLACED THE ANGLE IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA373](https://openairdocs.org/sdr/C2XA98IA373.md): Support · cracked · Sep 23, 1998 · N15730 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING UPPER SKIN SUPPORT AT RIB 8, SECOND FROM FORWARD, CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA289](https://openairdocs.org/sdr/C2XA98IA289.md): Control Cable · frayed · Jul 29, 1998 · N15730 · Emb EMB120RT · Aileron Control System > SHV - FLT 3776 - THE PILOT REPORTED THE LEFT CONTROL YOKE HAD EXCESSIVE PLAY IN AILERON CONTROL. THE AIRCRAFT LANDED AT SHV WITHOUT INCIDENT WHERE MAINTENANCE FOUND THE LEFT AILERON CONTROL QUADRANT LOWER CABLE TO HAVE BROKEN STRANDS. MAINTENANCE REMOVED AND - [SDR C2XA98CL014](https://openairdocs.org/sdr/C2XA98CL014.md): Annunciator · failed · Feb 19, 1998 · N15730 · Emb EMB120RT · Trailing Edge Flap Control System > CLE - FLT 3143 - CREW REPORTED DURING CLIMB RECEIVED A FLAP FAULT, AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTNENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE FLAP ANNUNCIATOR ASSEMBLE IAW EMB-120 MM 27-50-05. OPERATIONAL CHECKS WE - [SDR C2XA97CL081](https://openairdocs.org/sdr/C2XA97CL081.md): Brake Disk · broken · Oct 21, 1997 · N15730 · Emb EMB120RT · Brake > CLE - FLT 3313 - CREW REPORTED THAT WHILE THEY WERE TAXING AIRCRAFT TO THE RUNWAY THE NR 2 BRAKE LOCKED UP. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR 2 BRAKE TO HAVE A BROKEN DISK. THE NR 2 BRAKE WAS REMOVED AND REPLACED IAW EMB 120 MM 32-41-05, OP - [SDR C2XA97CL002](https://openairdocs.org/sdr/C2XA97CL002.md): Actuator · malfunctioned · Jan 3, 1997 · N15730 · Emb EMB120RT · Landing Gear Actuator > CLE - FLT 3045 - CREW REPORTED, THAT AFTER TAKEOFF THE LEFT MAIN LANDING GEAR WOULD NOT RETRACT, THE GEAR WAS CYCLED THREE TIMES WITH THE SAME RESULTS. AIRCRAFT RETURNED TO BASE. MAINTENANCE ADJUSTED THE SEQUENCE VALVE, TEST FLGHT NR 9493 UNSATISFACTORY. MA - [SDR C2XA96CL033](https://openairdocs.org/sdr/C2XA96CL033.md): Engine · oil leak · Sep 16, 1996 · N15730 · Emb EMB120RT · Turbine Engine Oil System > CLE - DURING A ROUTINE LINE CHECK INSPECTION, MAINTENANCE FOUND THE LEFT ENGINE TO HAVE ENGINE OIL LEAKING OUT OF THE INLET DUE TO INTERNAL LEAK. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE IAW CONTINENTAL EXPRESS MX DIRECTIVES NR 7, NR 8, AND NR 9. ALL - [SDR C2XA95IA362](https://openairdocs.org/sdr/C2XA95IA362.md): Support · cracked · Nov 15, 1995 · N15730 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 20, NR 3 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA361](https://openairdocs.org/sdr/C2XA95IA361.md): Support · cracked · Nov 15, 1995 · N15730 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 18, NR 3 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA360](https://openairdocs.org/sdr/C2XA95IA360.md): Support · cracked · Nov 15, 1995 · N15730 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 18, NR 4 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA359](https://openairdocs.org/sdr/C2XA95IA359.md): Support · cracked · Nov 15, 1995 · N15730 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 18, NR 5 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA358](https://openairdocs.org/sdr/C2XA95IA358.md): Support · cracked · Nov 15, 1995 · N15730 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 18, NR 2 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA357](https://openairdocs.org/sdr/C2XA95IA357.md): Support · cracked · Nov 15, 1995 · N15730 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 18, NR 3 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) Next page: https://openairdocs.org/deregistered/N15730-2007-10-25/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N15730' AND deregistration_id = 'N15730-2007-10-25' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N15730-2007-10-25/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.